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Effects of periodic excitation on turbulent flow separation from a flap
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On the delay of airfoil stall by periodic excitation
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Oscillatory control of separation at high Reynolds numbers
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Active flow separation control on wall-mounted hump at high Reynolds numbers
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Seifert, A., and Pack, L. G., "Active Flow Separation Control on Wall-Mounted Hump at High Reynolds Numbers," AIAA Journal, Vol. 40, No. 7, 2002, pp. 1363-1372.
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Active control of separation from the slat shoulder of a supercritical airfoil
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Pack, L. G., Schaeffler, N. W., Yao, C., and Seifert, A., "Active Control of Separation from the Slat Shoulder of a Supercritical Airfoil," Journal of Aircraft (to be published).
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Journal of Aircraft
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Pack, L.G.1
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Active separation control: Fundamental principles, current status and future directions
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Seifert, A.1
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Study of the application of separation control by unsteady excitation to civil transport aircraft
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Stoner, R.C.3
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Feifel, G.E.5
Feifel, W.M.6
Rush, H.M.7
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Parametric investigation of a high-lift airfoil at high Reynolds numbers
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Active control of cylinder flow with and without a splitter plate using piezoelectric actuators
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Naim, A., Greenblatt, D., Seifert, A., and Wygnanski, I., "Active Control of Cylinder Flow with and Without a Splitter Plate Using Piezoelectric Actuators," AIAA Paper 2002-3070, June 2002.
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Naim, A.1
Greenblatt, D.2
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M.S. Thesis, Dept. of Fluid Mechanics and Heat Transfer, Tel-Aviv Univ., Ramat-Aviv, Israel, March
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Naim, A., "Active Control of Cylinder Flow with and Without a Splitter Plate," M.S. Thesis, Dept. of Fluid Mechanics and Heat Transfer, Tel-Aviv Univ., Ramat-Aviv, Israel, March 2003.
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Naim, A.1
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